# Service difficulty reports: N518AU, cancelled Oct 10, 2008

A list on [N518AU, cancelled Oct 10, 2008](https://openairdocs.org/deregistered/N518AU-2008-10-10.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 88 reports

- [SDR USAA920081294](https://openairdocs.org/sdr/USAA920081294.md): Skin · cracked · Jul 8, 2008 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT RON MAJOR REPAIR LOG 4390633- FUSELAGE SKIN CRACKED AT BS 727E, S-24R. REPAIRED FUSELAGE SKIN AT BS727E, S-24R IAW B737 SRM 53-00-01 AND US AIRWAYS TYPICAL REPAIR 53-33. (B)
- [SDR USAA920070820](https://openairdocs.org/sdr/USAA920070820.md): Stringer · corroded · Sep 8, 2007 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON STRINGER, BS 1006 - BS 1016, RBL 8. REPAIRED STRINGER, BS 1006 - BS 1016, RBL 8 IAW B737-300 SRM 51-10-02.
- [SDR USAA920070821](https://openairdocs.org/sdr/USAA920070821.md): Floorbeam · corroded · Sep 7, 2007 · N518AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - MAJOR REPAIR - C-5 CHECK, LEVEL 2 CORROSION ON FLOORBEAM, BS 986, LBL 10. REPAIRED FLOORBEAM, BS 986, LBL 10 IAW USAIRWAYS TYPICAL REPAIR 53-10-05B.
- [SDR USAA920070819](https://openairdocs.org/sdr/USAA920070819.md): Fitting · cracked · Sep 7, 2007 · N518AU · Boeing 7373B7 · Horizontal Stabilizer Miscellaneous Structure
  > CLT - MAJOR REPAIR - C-5 CHECK, LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING CRACKED, STABILIZER STATION 83.05. REPLACED LEFT HAND HORIZONTAL STABILIZER CENTER SECTION THRUST BEAM CORNER FITTING, STABILIZER STATION 83.05 IAW B737-
- [SDR USAA920070887](https://openairdocs.org/sdr/USAA920070887.md): Skin · cracked · Sep 4, 2007 · N518AU · Boeing 7373B7 · Service Doors
  > CLT - MAJOR REPAIR - C-5 CHECK, FORWARD SERVICE DOOR EXTERIOR SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED FORWARD SERVICE DOOR EXTERIOR SKIN AT UPPER HINGE CUTOUT IAW USAIRWAYS TYPICAL REPAIR 52-10-13.
- [SDR USAA070497](https://openairdocs.org/sdr/USAA070497.md): Frame · cracked · Jun 28, 2007 · N518AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND BS 847 RBL 36. REPAIRED PER SRM 51-40-02, DEFECT SIZE: 1/16".
- [SDR SB07045](https://openairdocs.org/sdr/SB07045.md): Wire · broken · Jun 7, 2007 · N518AU · Boeing 7373B7 · Light System Wiring
  > PIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC BROKEN/INOPERATIVE. MAINTENANCE REPAIRED WIRES ON SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7ABC. OPERATIONAL CHECK GOOD.
- [SDR USAA200704005](https://openairdocs.org/sdr/USAA200704005.md): Skin · cracked · Apr 23, 2007 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CRACK FOUND AT STA 727D + 18" AND S24L. INSTALLED DOUBLER PER SRM 53-00-01 AND TR 53-60-03A.
- [SDR USAA061216](https://openairdocs.org/sdr/USAA061216.md): Door Frame · cracked · Oct 13, 2006 · N518AU · Boeing 7373B7 · Fuselage Main, Structure
  > FWD CARGO DOOR FWD FRAME AT LOWER DOOR STOP BS 440 S23R CRACK. INSTALLED DOUBLER AND FILLERS IAW EA 98153, DEFECT SIZE:.25 INCH.
- [SDR SB06084](https://openairdocs.org/sdr/SB06084.md): Battery Pack · discharged · Aug 29, 2006 · N518AU · Boeing 7373B7 · Emergency Lighting
  > DCA - MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR SB06066](https://openairdocs.org/sdr/SB06066.md): Windshield · cracked · Jul 7, 2006 · N518AU · Boeing 7373B7 · Flight Compartment Windows
  > PIT FLT288 DURING CRUISE, EN ROUTE FROM CLT TO YYZ, THE OUTER PANE OF THE CAPTAIN'S L1 WINDSHIELD SHATTERED. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD PE
- [SDR SB06020](https://openairdocs.org/sdr/SB06020.md): Cable · misrouted · Feb 22, 2006 · N518AU · Boeing 7373B7 · Escape Slide
  > DURING FAA RAMP INSPECTION, FAA FOUND THE R2 DOOR ESCAPE SLIDE DEPLOY CABLE ROUTED INCORRECTLY. MAINTENANCE REROUTED THE R2 DOOR ESCAPE SLIDE CABLE (LATCH ASSEMBLY) PER MM 25-61-35. REINSTALLED R2 DOOR ESCAPE SLIDE PER MM 25-61-35-402-003.
- [SDR USAA051389](https://openairdocs.org/sdr/USAA051389.md): Stiffener · cracked · Nov 15, 2005 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT END OF LT PACK BAY AT I/B AFT CORNER CRACKED. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWG 65-45402. DEFECT SIZE: 1 INCH CRACK.
- [SDR USAA050060](https://openairdocs.org/sdr/USAA050060.md): Skin · delaminated · Jan 1, 2005 · N518AU · Boeing 7373B7 · Wing, Plate/Skin
  > PIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 6 INCH AREA, BOTTOM SIDE 14 INCHES FROM INBOARD END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLERS AND FILLRS PER SRM 51-70-10. (M)
- [SDR USAA050024](https://openairdocs.org/sdr/USAA050024.md): Floorbeam · corroded · Jan 1, 2005 · N518AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT - FOUND CHORD AND ANGLE CORRODED AT SCREW HOLES, STATION 344 RBBL -13 TO LBBL -24. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED T-CAP, FABRICATED NEW CHORD AND ANGLE SPLICES, INSTALLED PER SRM 53-10-51. (M)
- [SDR USAA050061](https://openairdocs.org/sdr/USAA050061.md): Skin · delaminated · Jan 1, 2005 · N518AU · Boeing 7373B7 · Wing, Plate/Skin
  > PIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 4.5 INCH AREA, 34 INCHES FROM F/B EDGE. REMOVED DAMAGE, INSTALLED FILLERS, DOUBLERS PER SRM 51-70-10. (M)
- [SDR USAA041101](https://openairdocs.org/sdr/USAA041101.md): Strap · corroded · Dec 14, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K)
- [SDR USAA041100](https://openairdocs.org/sdr/USAA041100.md): Support · cracked · Dec 8, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - Q05 - SUPPORT,.075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM.
- [SDR USAA041067](https://openairdocs.org/sdr/USAA041067.md): Frame · corroded · Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG DWG 65C22910. (K)
- [SDR USAA041066](https://openairdocs.org/sdr/USAA041066.md): Mount · corroded · Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage, Equipment Attach Fittings
  > PIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)
- [SDR USAA041065](https://openairdocs.org/sdr/USAA041065.md): Mount · corroded · Dec 3, 2004 · N518AU · Boeing 7373B7 · Fuselage, Equipment Attach Fittings
  > PIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)
- [SDR USAA041071](https://openairdocs.org/sdr/USAA041071.md): Skin · chafed · Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - Q5 - SKIN, 9 INCHES X.5 INCH X.0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR SCHEME IAW SRM. (K)
- [SDR USAA041069](https://openairdocs.org/sdr/USAA041069.md): Intercostal · cracked · Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K)
- [SDR USAA041068](https://openairdocs.org/sdr/USAA041068.md): Skin · corroded · Dec 2, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K)
- [SDR USAA041072](https://openairdocs.org/sdr/USAA041072.md): Frame · corroded · Dec 1, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K)
- [SDR USAA041070](https://openairdocs.org/sdr/USAA041070.md): Frame · corroded · Dec 1, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORROSION, PRIMED AND PAINTED ISW SRM. (K)
- [SDR USAA041074](https://openairdocs.org/sdr/USAA041074.md): Floorbeam · corroded · Nov 24, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > PIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 13 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K)
- [SDR USAA041073](https://openairdocs.org/sdr/USAA041073.md): Skin · delaminated · Nov 22, 2004 · N518AU · Boeing 7373B7 · Trailing Edge Flaps
  > PIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K)
- [SDR USAA040981](https://openairdocs.org/sdr/USAA040981.md): Stringer · cracked · Nov 21, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - Q5 - STRINGER,.25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40-09, 51-30-01.
- [SDR USAA040979](https://openairdocs.org/sdr/USAA040979.md): Skin · cracked · Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537.
- [SDR USAA040978](https://openairdocs.org/sdr/USAA040978.md): Skin · bulged · Nov 18, 2004 · N518AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537.
- [SDR USAA040977](https://openairdocs.org/sdr/USAA040977.md): Skin · cracked · Nov 17, 2004 · N518AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - Q5 - NR 6 SLAT SKIN,.1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.
- [SDR USAA040980](https://openairdocs.org/sdr/USAA040980.md): Stringer · cracked · Nov 15, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - Q5 - STRINGER,.75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221.
- [SDR USAA040982](https://openairdocs.org/sdr/USAA040982.md): Tie · cracked · Nov 13, 2004 · N518AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART.
- [SDR USAA040983](https://openairdocs.org/sdr/USAA040983.md): Structure · cracked · Nov 10, 2004 · N518AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - Q5 - NR 4 SLAT, SEVERAL.1250 INCH TO.2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.
- [SDR USAA040843](https://openairdocs.org/sdr/USAA040843.md): Skin · cracked · Nov 7, 2004 · N518AU · Boeing 7373B7 · Leading Edge Devices
  > SKIN,.1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.
- [SDR USAA040984](https://openairdocs.org/sdr/USAA040984.md): Bulkhead · cracked · Nov 5, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 209 DETAIL II.
- [SDR USAA040631](https://openairdocs.org/sdr/USAA040631.md): Skin · cracked · Sep 21, 2004 · N518AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2.25 INCH,.5 INCH ABOVE STRINGER 25R SKIN LAP AT STATION 764. INSTALLED DOUBLER/TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M)
- [SDR SB04124](https://openairdocs.org/sdr/SB04124.md): Light · unsecure · Sep 16, 2004 · N518AU · Boeing 7373B7 · Emergency Lighting
  > PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 10A INOPERATIVE. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHTS ON SEAT 10A. OPERATIONAL CHECK GOOD.
- [SDR USA2004F00051](https://openairdocs.org/sdr/USA2004F00051.md): Outflow Valve · failed · May 5, 2004 · N518AU · Boeing 7373B7 · Pressure Regulator/Outflow Valve
  > ENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED.
- [SDR USA2004F00046](https://openairdocs.org/sdr/USA2004F00046.md): Controller · malfunctioned · May 5, 2004 · N518AU · Boeing 7373B7 · Cabin Pressure Controller
  > ENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WI
- [SDR USAASB04048](https://openairdocs.org/sdr/USAASB04048.md): Fan Blade · eroded · Apr 30, 2004 · N518AU · Boeing 7373B7 · Cabin Cooling System
  > IAH - FLT 775 - EN ROUTE FROM PHL-IAH, AT FL310, THE CABIN ALTITUDE CLIMBED VERY SLOWLY TO 9,500 FEET. AT THIS TIME, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN IMMEDIATE DESCENT OT FL240. CABIN ALTITUDE BEGAN TO DESCEND AND STABILIZE AT 3
- [SDR USAASB04018](https://openairdocs.org/sdr/USAASB04018.md): Door · out of rig · Feb 14, 2004 · N518AU · Boeing 7373B7 · Cargo/Baggage Doors
  > EN ROUTE AT FL330, A/C LOST PRESS. CREW ACCOMPLISHED RAPID DESCENT OT 10,000 FT. OXY MASKS DEPLOYED DURING DESCENT. STANDBY & MANUAL PRESS MODES USED BUT NOT EFFECTIVE. OUTFLOW VALVE REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND HEARD BENEATH THE FLOORBOA
- [SDR USA2004F00014](https://openairdocs.org/sdr/USA2004F00014.md): Cabin Pressure · failed · Feb 14, 2004 · N518AU · Boeing 7373B7 · Cabin Pressure Control System
  > ENROUTE, WHILE LEVEL AT FL330, THE AIRCRAFT LOST PRESSURIZATION. CREW ACCOMPLISHED A RAPID DESCENT TO 10,000 FT. OXYGEN MASKS DID DEPLOY DURING DESCENT. STANDBY AND MANUAL PRESSURIZATION MODES WERE USED BUT WERE NOT EFFECTIVE. OUTFLOW VALVE WAS REPORTED TO
- [SDR USAASB03215](https://openairdocs.org/sdr/USAASB03215.md): Door Seal · failed · Dec 14, 2003 · N518AU · Boeing 7373B7 · Doors
  > DURING CRUISE, EN ROUTE FROM IND-CLT AT FL290, A LOUD BANG WAS HEARD FROM THE FORWARD GALLEY AREA, FOLLOWED BY THE CABIN ALTITUDE CLIMBING UNCONTROLABLLY. CREW REPORTED THE OUTFLOW VALVE WAS IN THE FULL CLOSED POSITION. THE OXYGEN MASKS DEPLOYED AND BOTH TE
- [SDR USAASB03131](https://openairdocs.org/sdr/USAASB03131.md): Wire · broken · Aug 7, 2003 · N518AU · Boeing 7373B7 · Light System Wiring
  > ORD - MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY ON SEAT ROW 10, LEFT SIDE, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 10, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03118](https://openairdocs.org/sdr/USAASB03118.md): Fuse · blown · Jul 20, 2003 · N518AU · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE LEFT OVERWING HATCH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWER SUPPLY M1134 AND A BAD PLUG ON THE EMERGENCY SIGN. REPLACED FUSE AND PLUG. OPS CHECK GOOD. (M)
- [SDR USAASB03082](https://openairdocs.org/sdr/USAASB03082.md): Wire · faulty · Jun 14, 2003 · N518AU · Boeing 7373B7 · Light System Wiring
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTING AT SEAT 12 ABC WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED WIRING ON SEAT 12ABC PER STANDARD WIRING PRACTICES MANUAL 20-10-13. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03081](https://openairdocs.org/sdr/USAASB03081.md): Control Panel · faulty · Jun 12, 2003 · N518AU · Boeing 7373B7 · Cabin Pressure Control System
  > CLT - FLT 1254 - MCI TO CLT, AT FL350, CAPTAIN REPORTED A PRESSURIZATION PROBLEM, AS CABIN ALTITUDE INCREASED. CABIN ALTITUDE EXCEEDED 14,000 FT, THE OXYGEN MASKS AUTO DEPLOYED. AN EMERGENCY DESCENT TO FL100 WAS ACCOMPLISHED. THE FLT CONTINUED ONTO CLT, AT
- [SDR USAASB04004](https://openairdocs.org/sdr/USAASB04004.md): Seal · failed · Jan 3, 2003 · N518AU · Boeing 7373B7 · Cargo/Baggage Doors
  > DURING CLIMB-OUT FROM PHL, EN ROUTE TO ORD AT FL270, CRWE HEARD A LOUD BANG AND A BURST OF AIR. NO MASTER CAUTION WARNING OR DOOR WARNING LIGHTS ILLUMINATED. THE AUTO PRESSURZATION SYSTEM HAD FAILED AND WAS PLACED IN STANDBY. IN STANDBY, THE CABIN ALTITUDE

Next page: https://openairdocs.org/deregistered/N518AU-2008-10-10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N518AU' AND deregistration_id = 'N518AU-2008-10-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N518AU-2008-10-10/reports

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